JP2001090692A - Axial blower - Google Patents

Axial blower

Info

Publication number
JP2001090692A
JP2001090692A JP26737099A JP26737099A JP2001090692A JP 2001090692 A JP2001090692 A JP 2001090692A JP 26737099 A JP26737099 A JP 26737099A JP 26737099 A JP26737099 A JP 26737099A JP 2001090692 A JP2001090692 A JP 2001090692A
Authority
JP
Japan
Prior art keywords
rib
streamlined
blower
ribs
blade
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP26737099A
Other languages
Japanese (ja)
Other versions
JP4321690B2 (en
Inventor
Mitsuyoshi Ishijima
満義 石嶋
Tomoshi Shimizu
知史 清水
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toshiba Carrier Corp
Original Assignee
Toshiba Carrier Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toshiba Carrier Corp filed Critical Toshiba Carrier Corp
Priority to JP26737099A priority Critical patent/JP4321690B2/en
Publication of JP2001090692A publication Critical patent/JP2001090692A/en
Application granted granted Critical
Publication of JP4321690B2 publication Critical patent/JP4321690B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/384Blades characterised by form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/306Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the suction side of a rotor blade

Abstract

PROBLEM TO BE SOLVED: To provide an axial blower capable of lowering blowing noises while reducing the peeling of the flow to be generated in a blade negative pressure surface and improved in molding property thereof at a low cost. SOLUTION: Plural blades 13 are arranged in the periphery of a boss part 12, to which a rotary shaft is fixed. Plural streamlined ribs 14 smoothly continued from a front edge thereof toward a blade rear edge part 13d are arranged in each blade 13 at a negative pressure surface 13a side front edge part 13c along the outline of the front edge with the predetermined space in the radial direction of a blower. These streamlined ribs 14 are arranged in plural lines 14a, 14b with the predetermined space in the circumferential direction of the blower.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、例えば空気調和機
の室外ファンや換気装置等に好適な軸流送風機に係り、
特に、翼負圧面上の流れの剥離を抑制して送風性能の向
上と送風音の低減とを共に図った軸流送風機に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an axial blower suitable for, for example, an outdoor fan or a ventilator of an air conditioner.
In particular, the present invention relates to an axial blower that suppresses separation of a flow on a blade negative pressure surface to improve blowing performance and reduce blowing noise.

【0002】[0002]

【従来の技術】図13は従来の軸流送風機1の翼負圧面
側から見たときの正面図、図14は、その軸流送風機1
の翼1枚分を図示して他の翼を省略した一部切欠正面図
である。この軸流送風機1は、図示しない回転軸が中心
部Oに固定される円筒状のボス部2の外周側面に、複数
の翼3,3…を周方向に所定のピッチを置いて一体また
は一体的に形成している。各翼3は、図中矢印で示す送
風機回転方向(周方向)に対して空気流の上流側端部を
なす凹弧状の前縁部3aと、空気流の下流側端部をなす
後縁部3bと、凸弧状の外周端部3cと、図15でも示
す流体吸込側の負圧面3dと、その裏面側の正圧面3e
とを有する。
2. Description of the Related Art FIG. 13 is a front view of a conventional axial flow blower 1 as viewed from the blade negative pressure side, and FIG.
FIG. 6 is a partially cutaway front view illustrating one wing and omitting other wings. The axial blower 1 is configured such that a plurality of blades 3, 3... Are integrally or integrally formed on a peripheral side surface of a cylindrical boss portion 2 having a rotating shaft (not shown) fixed to a central portion O at a predetermined pitch in a circumferential direction. Is formed. Each wing 3 has a concave arc-shaped leading edge 3a that forms an upstream end of the airflow with respect to the blower rotation direction (circumferential direction) indicated by an arrow in the drawing, and a rear edge that forms a downstream end of the airflow. 3b, a convex arc-shaped outer peripheral end 3c, a suction surface 3d on the fluid suction side also shown in FIG. 15, and a pressure surface 3e on the back surface thereof.
And

【0003】そして、各翼3の負圧面3d側の前縁部3
aの厚さを後縁部よりも厚い流線形の厚肉部3fに形成
すると共に、この流線形厚肉部3fの前縁部3a上に、
正面形状がほぼ矩形の複数の流線形リブ4を前縁部3a
の輪郭線(外形線)に沿って送風機半径方向に所定間隔
を置いて列状に配設している。
[0003] The leading edge 3 of each blade 3 on the suction side 3d side.
a is formed on the streamline thick portion 3f which is thicker than the trailing edge, and on the front edge 3a of the streamline thick portion 3f,
A plurality of streamline ribs 4 having a substantially rectangular front shape are connected to the front edge 3a.
Are arranged in a row at predetermined intervals in the radial direction of the blower along the contour line (outline).

【0004】図15は図12で示すようにボス部2の中
心部に固定される図示しない回転軸の軸心Oから半径方
向に任意の距離r離れた部分における周方向の翼断面を
示している。
FIG. 15 shows a circumferential cross section of a blade in a portion at an arbitrary distance r in the radial direction from an axis O of a rotating shaft (not shown) fixed to the center of the boss portion 2 as shown in FIG. I have.

【0005】この図15に示すように各翼3の負圧面3
d側の前縁部3aには、流線形厚肉部3fが形成され、
しかもその流線形厚肉部3f上には複数の流線形リブ4
を配設しているので、この翼負圧面3d側前縁部3aか
ら流入した空気流れUが流線形リブ4を通風した後に縦
渦列Uzになる。このために、負圧面3dから空気流れ
が剥離するのを抑制することができるので、後縁部3b
の後方(下流)に発生する後流渦fuの幅を縮小して送
風音を低減させることができる。
[0005] As shown in FIG.
A streamline thick portion 3f is formed on the leading edge 3a on the d side,
Moreover, a plurality of streamline ribs 4 are provided on the streamline thick portion 3f.
Is disposed, the air flow U flowing from the blade-side negative pressure surface 3d side leading edge 3a passes through the streamlined rib 4 and becomes a vertical vortex street Uz. For this reason, it is possible to suppress the air flow from separating from the negative pressure surface 3d, so that the trailing edge portion 3b
The width of the wake vortex fu generated behind (downstream) the air can be reduced.

【0006】[0006]

【発明が解決しようとする課題】しかしながら、このよ
うな従来の軸流送風機1では、流線形リブ4が1列しか
配列されていないので、送風音低減効果が必ずしも十分
ではないという課題がある。
However, in such a conventional axial-flow blower 1, there is a problem that the airflow noise reduction effect is not always sufficient because only one row of streamlined ribs 4 is arranged.

【0007】本発明はこのような事情を考慮してなされ
たもので、その目的は、翼負圧面で発生する流れの剥離
をさらに低減して送風音をさらに低減することができる
安価で成形性の良好な軸流送風機を提供することにあ
る。
The present invention has been made in view of such circumstances, and an object of the present invention is to provide an inexpensive and compact mold that can further reduce the flow separation generated on the negative pressure surface of the blade and further reduce the blowing noise. And to provide a good axial flow blower.

【0008】[0008]

【課題を解決するための手段】請求項1に係る発明は、
回転軸が固定されるボス部の外周に、複数の翼を配設し
た軸流送風機において、上記各翼の負圧面側前縁部に、
その前縁から翼後縁に向けて滑かに連なる流線形リブの
複数を、送風機半径方向に所定の間隔を置いて上記前縁
の輪郭線に沿って列状に配設し、この流線形リブ列を送
風機周方向に所定の間隔を置いて複数列設けたことを特
徴とする軸流送風機である。
The invention according to claim 1 is
In the axial flow blower in which a plurality of blades are arranged on the outer periphery of the boss portion to which the rotation shaft is fixed, at the suction surface side front edge of each of the blades,
A plurality of streamlined ribs smoothly connected from the leading edge toward the blade trailing edge are arranged in a row along the contour of the leading edge at predetermined intervals in the radial direction of the blower. An axial blower characterized in that a plurality of rib rows are provided at predetermined intervals in a circumferential direction of the blower.

【0009】請求項2に係る発明は、翼前縁側の外側流
線形リブ列よりも送風機周方向内側に設けた内側流線形
リブ列の各流線形リブは、その流入空気の通風方向を案
内する通風側面の角度θaを、上記外側流線形リブ列の
通風側面の角度θbに対して12°〜18°の範囲で傾
斜させていることを特徴とする請求項1記載の軸流送風
機である。
According to a second aspect of the present invention, each streamlined rib of the inner streamlined rib array provided on the inner side in the circumferential direction of the blower with respect to the outer streamlined rib array on the blade leading edge side guides the ventilation direction of the inflow air. 2. The axial blower according to claim 1, wherein the angle θa of the ventilation side surface is inclined in a range of 12 ° to 18 ° with respect to the angle θb of the ventilation side surface of the outer streamline rib row.

【0010】請求項3に係る発明は、内側流線形リブ列
の各流線形リブは、回転軸中心Oと、翼外周と翼後縁と
の交点Qと、を結ぶ線分OQに対して各々の所定角度で
それぞれ傾斜させ、これらの各傾斜角を翼外周からボス
部側の流線形リブに行くに従って大きくすることを特徴
とする請求項1または2記載の軸流送風機である。
According to a third aspect of the present invention, each streamlined rib in the inner streamlined rib row is defined by a line segment OQ connecting the center of rotation axis O and an intersection Q between the blade outer periphery and the blade trailing edge. The axial flow blower according to claim 1 or 2, wherein each of the inclinations is increased at a predetermined angle from the outer periphery of the blade to the streamline rib on the boss side.

【0011】請求項4に係る発明は、内側流線形リブ列
は、その各流線形リブを送風機半径方向に等間隔で配置
する一方、これらの各流線形リブの送風機周方向に沿う
長さLを、外側流線形リブ列の各流線形リブの送風機
周方向に沿う長さLに対し、ほぼ0.8Lの長さに
形成していることを特徴とする請求項1〜3のいずれか
1項に記載の軸流送風機である。
According to a fourth aspect of the present invention, in the inner streamlined rib array, the streamlined ribs are arranged at regular intervals in the radial direction of the blower, and the length L of each streamlined rib along the circumferential direction of the blower is set. 2, with respect to the length L 1 along the fan circumferential direction of the aerodynamic ribs of the outer flow linear rib rows, according to claim 1, wherein the forming substantially the length of 0.8 L 1 An axial flow blower according to any one of the preceding claims.

【0012】請求項5に係る発明は、内側流線形リブ列
は、その流線形リブを、外側流線形リブ列の流線形リブ
同士の間隙に対応する位置に配設していることを特徴と
する請求項1〜4のいずれか1項に記載の軸流送風機で
ある。
The invention according to claim 5 is characterized in that the inner streamline rib row is disposed at a position corresponding to the gap between the streamline ribs of the outer streamline rib row. The axial blower according to any one of claims 1 to 4.

【0013】請求項6に係る発明は、内側流線形リブ列
の各流線形リブは、その送風機周方向各前縁を、外側流
線形リブ列の各流線形リブの送風機周方向各前縁を結ぶ
円弧曲線の中心をP、その半径をrとしたときに、そ
の中心Pと同心でかつ半径r よりも大きい半径r
円弧線上に位置させていることを特徴とする請求項1〜
5のいずれか1項に記載の軸流送風機である。
According to a sixth aspect of the present invention, there is provided an inner streamlined rib array.
Each streamlined rib has its front edge in the circumferential direction
Connect each leading edge of each streamlined rib in the linear rib row in the circumferential direction of the blower
P is the center of the arc curve and r is its radius1And when
Concentric with the center P and radius r 1Radius r greater than2of
3. The method according to claim 1, wherein the first and second radiators are positioned on an arc line.
Item 5. The axial blower according to any one of Items 5.

【0014】請求項7に係る発明は、内,外両側の流線
形リブ列の各流線形リブは、その送風機半径方向に沿う
幅がみなほぼ同一幅に形成されていることを特徴とする
請求項1〜6のいずれか1項に記載の軸流送風機であ
る。
The invention according to claim 7 is characterized in that each streamline rib of the streamline rib rows on both the inner and outer sides is formed to have substantially the same width along the radial direction of the blower. Item 7. The axial flow blower according to any one of Items 1 to 6.

【0015】請求項8に係る発明は、内側流線形リブ列
の各流線形リブは、その送風機周方向に沿う断面の外面
が円弧面をなし、その円弧外面の翼前縁側一部の円弧曲
面の半径Raの方が、その反対側他部の円弧曲面の半径
Rbよりも大きくなるように一体に形成されていること
を特徴とする請求項1〜7のいずれか1項に記載の軸流
送風機である。
According to an eighth aspect of the present invention, in each streamline rib of the inner streamline rib row, an outer surface of a cross section along a circumferential direction of the blower forms an arc surface, and an arc curved surface of a part of the arc outer surface on the blade leading edge side. The axial flow according to any one of claims 1 to 7, wherein the radius Ra is integrally formed so as to be larger than the radius Rb of the arc-shaped curved surface at the other part on the opposite side. It is a blower.

【0016】請求項9に係る発明は、内側流線形リブ列
の各流線形リブは、その翼厚方向に沿う断面高さを、ボ
ス部側から翼外周方向に行くに従って漸次薄くなる翼前
縁部断面の厚さとは逆にボス部側から翼外周側に行くに
従って漸次高くなるように除変させると共に、上記翼外
周に最も近い流線形リブの高さをhとし、上記ボス部
に最も近い流線形リブの高さをhとしたときに、h
=2hとなるように設定されていることを特徴とする
請求項1〜8のいずれか1項に記載の軸流送風機であ
る。
According to a ninth aspect of the present invention, in each of the streamline ribs of the inner streamline rib array, the cross-sectional height along the blade thickness direction is gradually reduced from the boss toward the blade outer periphery. with removal strange is allowed to become gradually higher toward the blade outer peripheral side from the boss portion side opposite to the thickness of the part cross-section, the height of the nearest streamlined rib to the wing outer periphery and h 1, most to the boss aerodynamic rib height is taken as h 2 close, h 1
= It is an axial flow fan according to any one of claims 1 to 8, wherein it is set such that 2h 2.

【0017】これらの各発明によれば、軸流送風機の回
転により各翼がボス部の軸心周りに回転すると、各翼の
負圧面側の前縁部に、その外方から流入した空気流れが
複数列の流線形リブをそれぞれ通過して縦渦列となるの
で、翼負圧面上で層流境界層から乱流境界層に遷移され
る。この乱流境界層は層流境界層よりも気流の流れの剥
離が発生しにくいうえに、送風音の原因をなす後流渦の
幅を狭くするので、送風音を低減することができる。し
かも、上記流線形リブが通風方向に複数列あるので、上
記図13等で示す流線形リブが1列しかない従来例より
も、送風音の原因をなす後流渦の幅をさらに狭くするこ
とができる。このために、送風音をさらに低減すること
ができる。さらに、各流線形リブは各翼に例えば樹脂モ
ールド成型等により簡単に一体成形できるので、成形性
が良好であり、製造コストを低減できる。
According to each of these inventions, when each blade rotates around the axis of the boss by the rotation of the axial blower, the air flowing from the outside into the front edge on the negative pressure side of each blade. Passes through a plurality of rows of streamlined ribs to form a vertical vortex street, so that a transition is made from the laminar boundary layer to the turbulent boundary layer on the blade suction surface. In the turbulent boundary layer, separation of the airflow is less likely to occur than in the laminar boundary layer, and the width of the wake vortex that causes the blowing noise is narrowed, so that the blowing noise can be reduced. Moreover, since the streamlined ribs are arranged in a plurality of rows in the ventilation direction, the width of the wake vortex that causes the blowing noise is further reduced as compared with the conventional example in which the streamlined ribs shown in FIG. Can be. For this reason, the blowing noise can be further reduced. Furthermore, since each streamline rib can be easily formed integrally with each blade by, for example, resin molding, the moldability is good and the manufacturing cost can be reduced.

【0018】また、これらの発明のうち、請求項4〜8
の発明によれば、翼負圧面上で縦渦列を安定して発生さ
せることができるので、送風音の低減効果をさらに増大
させることができる。
Further, of these inventions, claims 4 to 8
According to the invention, since the vertical vortex street can be stably generated on the blade negative pressure surface, the effect of reducing the blowing noise can be further increased.

【0019】さらに、請求項9の発明によれば、各流線
形リブの高さと、翼前縁部の厚さを含めた前縁部の断面
厚さが送風機半径方向のいずれの箇所においてもほぼ等
しくなるので、この軸流送風機を樹脂モールド成形によ
り一体成形する際には、肉ひけを防止することができる
うえに、冷却時間を短縮することができるので、成形コ
ストを低減することができる。
According to the ninth aspect of the present invention, the height of each streamlined rib and the cross-sectional thickness of the leading edge including the thickness of the leading edge of the blade are substantially equal at any point in the radial direction of the blower. Therefore, when the axial blower is integrally molded by resin molding, the axial blower can be prevented from being thinned, and the cooling time can be shortened, so that the molding cost can be reduced.

【0020】[0020]

【発明の実施の形態】以下、本発明の実施形態を図1〜
図12に基づいて説明する。なお、これらの図中、同一
または相当部分には同一符号を付している。
BRIEF DESCRIPTION OF THE DRAWINGS FIG.
This will be described with reference to FIG. In these figures, the same or corresponding parts are denoted by the same reference characters.

【0021】図1は本発明の一実施形態に係る軸流送風
機11を翼負圧面側から見たときの全体構成を示す正面
図、図2はその翼1枚分を図示して他の翼を図示省略し
て示す一部切欠正面図である。これらの図に示すように
軸流送風機11は円筒状のボス部12の外周側面に、複
数の翼13,13,13を例えば周方向等分位置にて一
体ないし一体的に取り付けており、例えば樹脂モールド
成形等により一体に成形される。
FIG. 1 is a front view showing the entire configuration of an axial blower 11 according to an embodiment of the present invention as viewed from the blade suction side, and FIG. 2 is a view showing one blade and other blades. FIG. 2 is a partially cutaway front view showing the illustration. As shown in these figures, the axial blower 11 has a plurality of blades 13, 13, 13 integrally or integrally attached to the outer peripheral side surface of a cylindrical boss portion 12 at, for example, circumferentially equal positions. It is integrally formed by resin molding or the like.

【0022】ボス部12は有底円筒状の本体12aの内
部中心部に、図示しない駆動モータの回転軸を挿入させ
て固定するための小円筒状のボス12bと、このボス1
2bから放射状に延びてボス本体12aの内周面に一体
に連結するほぼ逆Y字状の連結リブ12cとを一体に連
成している。
The boss portion 12 has a small cylindrical boss 12b for inserting and fixing a rotating shaft of a drive motor (not shown) in the center of the inside of the bottomed cylindrical main body 12a.
A substantially inverted Y-shaped connecting rib 12c extending radially from 2b and integrally connected to the inner peripheral surface of the boss main body 12a is integrally connected.

【0023】一方、各翼13は、空気吸込側の負圧面1
3aと、その裏面の送風側である正圧面13bと、図
1,図2中矢印で示す送風機回転方向に対し、各翼13
の空気流の上流側端部をなす凹弧状の前縁部13cと、
空気流の下流側端部をなす後縁部13dと、これら前縁
部13cと後縁部13dの径方向外端同士を一体に連結
してなる凸弧状の外周端部13eとを一体に形成してい
る。
On the other hand, each blade 13 has a suction surface 1 on the air suction side.
3a, a positive pressure surface 13b, which is a blow side on the back surface, and each blade 13 with respect to a blower rotation direction indicated by an arrow in FIGS.
A concave front edge 13c forming an upstream end of the airflow of
A trailing edge portion 13d serving as a downstream end portion of the airflow and a convex arc-shaped outer peripheral end portion 13e formed by integrally connecting radially outer ends of the leading edge portion 13c and the trailing edge portion 13d are integrally formed. are doing.

【0024】そして、各翼13は、負圧面13a側の前
縁部13c上に、正面形状がほぼ長方形で前縁部13c
の前縁(前端)から後縁部13d方向に向けて滑かに連
なる複数の流線形リブ14を送風機半径方向に等間隔を
置いて各前縁部13cの輪郭線(外形線)に沿って、列
状に配置することにより外側流線形リブ列14aを形成
している。さらに、この外側流線形リブ列14aよりも
送風機周方向後縁部13d側(つまり翼内面側)へ所定
間隔離れた箇所において、複数の流線形リブ14を送風
機半径方向に所定の等間隔を置いて列状に配設して内側
流線形リブ列14bを形成し、これら内,外側流線形リ
ブ列14b,14aを並列に設けている。
Each wing 13 has a substantially rectangular front surface and a front edge 13c on the front edge 13c on the side of the suction surface 13a.
A plurality of streamlined ribs 14 smoothly connected from the front edge (front end) to the rear edge 13d in the blower radial direction at equal intervals along the contour (outline) of each front edge 13c. The outer streamlined rib row 14a is formed by arranging the outer streamlined rib rows 14a. Further, a plurality of streamlined ribs 14 are arranged at predetermined equal intervals in the radial direction of the blower at a predetermined distance from the outer streamline rib row 14a toward the trailing edge 13d in the circumferential direction of the fan (that is, the inner surface of the blade). The inner streamlined rib rows 14b are formed in a row, and the inner and outer streamlined rib rows 14b and 14a are provided in parallel.

【0025】そして、図2に示すように内側流線形リブ
列14bの各流線形リブ14は、その空気流れの通風方
向を案内する通風側面14bを、その外側近傍の外側
流線形リブ列14aの各流線形リブ14の通風側面14
に対して角度θで傾斜させており、その角度θとし
ては例えば12°〜18°の範囲に設定されている。
[0025] Each aerodynamic ribs 14 of the inner flow linear ribs column 14b as shown in FIG. 2, the ventilation side 14b 1 for guiding the airflow direction of the air flow, the outer flow linear ribs column 14a of the outer vicinity Ventilation side 14 of each streamline rib 14
and it is inclined at an angle θ with respect to a 1, as the the angle θ is set in a range of for example 12 ° ~ 18 °.

【0026】また、図3に示すように内側流線形リブ列
14bの各流線形リブ14の通風側面14bは、送風
機回転中心、すなわちボス部12の中心Oと、翼後縁部
13dの後縁と翼外周13eとの交点Qと、を結ぶ線分
OQに対しても、各所定角度α,α,α…α
傾斜している。しかも、これら傾斜角度α〜αは、
翼外周13eに最も近い流線形リブ14の通風側面14
の角度αからボス部12に最も近い流線形リブ1
4の通風側面14bの角度αnに行くに従って漸次傾
斜角度が大きくなり、α=2αに設定されている。
Further, the ventilation side 14b 1 of each aerodynamic ribs 14 of the inner flow linear ribs column 14b as shown in FIG. 3, blower rotational center, i.e. the center O of the boss portion 12, after the trailing edge portion 13d The line OQ connecting the edge and the intersection point Q of the blade outer periphery 13e is also inclined at predetermined angles α 1 , α 2 , α 3 ... Α n . Moreover, these inclination angles α 1 to α n are:
Vent side 14 of streamlined rib 14 closest to blade periphery 13e
b 1 angle α closest streamlined ribs 1 from 1 on the boss portion 12
Gradually inclined angle toward the angle αn of the ventilation side 14b 1 of 4 increases, is set to α n = 2α 1.

【0027】図4はこのように構成された軸流送風機1
1の翼負圧面13a側の空気流れUの状態を矢印線で示
している。図5は図4で示すようにボス部2の中心から
半径方向に所定距離r離れた翼13の任意箇所におい
て送風機周方向に切断したときの翼断面と、その翼断面
を流れる空気流れUの状態を示している。これらの図
中、矢印線は空気の流れ方向を示し、矢印線の回転は縦
渦列Uzを表している。
FIG. 4 shows an axial blower 1 constructed as described above.
The state of the air flow U on the side of the first blade negative pressure surface 13a is indicated by an arrow line. Figure 5 is a blade section when cut to the blower circumferential direction at any position of a predetermined distance r 1 apart blades 13 in the radial direction from the center of the boss portion 2 as shown in Figure 4, the air flow U flowing through the airfoil section The state of is shown. In these figures, the arrow lines indicate the flow direction of the air, and the rotation of the arrow lines indicates the vertical vortex street Uz.

【0028】これら図4,図5に示すように、上記軸流
送風機11では、その前縁部13cの前縁フィレットか
ら翼負圧面13a上に流入した空気流れUが外側流線形
リブ列14aと内側流線形リブ列14bとをそれぞれ通
過して、縦渦列Uzとなり、翼負圧面13a上を層流境
界層から乱流境界層に遷移させる。これにより、送風音
の原因をなす後流渦fzの幅を狭くして送風音を低減さ
せることができる。
As shown in FIGS. 4 and 5, in the axial flow blower 11, the air flow U flowing from the leading edge fillet of the leading edge portion 13c onto the blade suction surface 13a is transmitted to the outer streamlined rib row 14a. It passes through the inner streamlined rib row 14b and becomes a longitudinal vortex row Uz, and transitions from the laminar boundary layer to the turbulent boundary layer on the blade suction surface 13a. Thereby, the width of the wake vortex fz which causes the blowing sound can be narrowed to reduce the blowing sound.

【0029】しかも、この軸流送風機11によれば、流
線形リブ14のリブ列が内,外2列14b,14aある
ので、この内,外流線形リブ列14b,14aを空気流
れUが通過することにより翼負圧面13a上で2重に縦
渦列Uzを発生させることができる。このために、流線
形リブ14が1列しかない例えば図13で示す従来の軸
流送風機1よりも縦渦列Uzの発生量を増大させること
ができるので、送風音の原因である後流渦fzの幅をさ
らに狭くすることとができ、その分、送風量をさらに低
減することができる。なお、上記流線形リブ14bは3
列以上設けてもよい。
Moreover, according to the axial blower 11, since the streamlined ribs 14 have two inner and outer rows 14b and 14a, the air flow U passes through the inner and outer streamlined rib rows 14b and 14a. Thereby, the vertical vortex street Uz can be generated twice on the blade negative pressure surface 13a. For this reason, the generation amount of the vertical vortex row Uz can be increased as compared with, for example, the conventional axial flow fan 1 shown in FIG. The width of fz can be further reduced, and the amount of air blow can be further reduced. The streamline rib 14b is 3
More than one row may be provided.

【0030】そして、図6に示すように上記内側流線形
リブ列14bは、その各流線形リブ14の送風機周方向
に沿う長手方向の長さLを、外側流線形リブ列14a
の各流線形リブ14の送風機周方向に沿う長手方向の長
さLよりも短かく形成し、例えば0.8Lに形成し
ている。また、内側流線形リブ列14bの各流線形リブ
14の径方向の間隔Wをほぼ等間隔に設定している。
[0030] Then, the inner flow linear ribs column 14b as shown in FIG. 6, the longitudinal length L 2 along the fan circumferential direction of the aerodynamic ribs 14, the outer flow linear rib row 14a
It is formed shorter, formed for example in 0.8 L 1 than the longitudinal length L 1 along the fan circumferential direction of the aerodynamic ribs 14. In addition, the radial intervals W of the streamline ribs 14 in the inner streamline rib row 14b are set to be substantially equal.

【0031】さらに、図7に示すように内側流線形リブ
列14bの各流線形リブ14を、外側流線形リブ列14
aの送風機半径方向で隣り合う流線形リブ14同士の間
隙に対応する位置に配設している。
Further, as shown in FIG. 7, each streamline rib 14 of the inner streamline rib row 14b is replaced with the outer streamline rib row 14b.
It is disposed at a position corresponding to the gap between the streamline ribs 14 adjacent to each other in the radial direction of the blower a.

【0032】さらにまた、図8に示すように、外側流線
形リブ列14aの各流線形リブ14の前縁(図8では右
端)同士を結ぶ仮想の円弧曲線15aの中心をP、その
半径をraとしたときに、その中心Pと同心でかつ半径
raよりも大径の半径rbの仮想の円弧曲線15b上
に、内側流線形リブ列14bの各流線形リブ14の前縁
が位置するように配置している。
Further, as shown in FIG. 8, the center of a virtual arc curve 15a connecting the leading edges (right ends in FIG. 8) of each streamline rib 14 of the outer streamline rib row 14a is P, and its radius is When ra is set, the front edge of each streamline rib 14 of the inner streamline rib row 14b is positioned on a virtual arc curve 15b concentric with the center P and having a radius rb larger than the radius ra. Has been placed.

【0033】また、図9に示すように外側流線形リブ列
14aにおける各流線形リブ14の送風機半径方向の幅
Waと、内側流線形リブ列14bにおける各流線形リブ
14の送風機半径方向の幅Wbとをほぼ同一幅に形成し
ている。
Further, as shown in FIG. 9, the radial width Wa of each streamline rib 14 in the outer streamline rib row 14a and the radial width of each streamline rib 14 in the inner streamline rib row 14b. Wb is formed to have substantially the same width.

【0034】図10は内側流線形リブ列14bの各流線
形リブ14を送風機周方向に沿って切断したときの円弧
状断面14cを示しており、この円弧状断面14cは、
その翼前縁部13c側の一部である前半部14c1の曲
率半径をrc、その他部である後半部14c2の曲率半
径をrdとしたときにrc>rdが成立するように形成
されている。
FIG. 10 shows an arc-shaped cross section 14c when each streamline rib 14 of the inner streamline rib row 14b is cut along the circumferential direction of the blower.
When the radius of curvature of the front half portion 14c1, which is a part of the wing front edge portion 13c side, is rc, and the radius of curvature of the rear half portion 14c2, which is the other portion, is rd, rc> rd is established.

【0035】ところで、図11に示すように各翼13の
前縁部13cの送風機半径方向に沿う翼断面の厚さh
はボス部12側Zaから翼外周13e側Zbへ行くに従
って漸次薄くなるように除変されている。
By the way, as shown in FIG. 11, the thickness h 0 of the blade section of the leading edge 13c of each blade 13 along the radial direction of the blower.
Is gradually reduced from the boss 12 side Za to the blade outer periphery 13e side Zb.

【0036】一方、図12に示すように各流線形リブ1
4の高さは、ボス部12側Yaから翼外周13e側Yb
へ行くに従って漸次高くなるように徐変されており、翼
外周13eに最も近い流線形リブの高さhと、ボス部
12に最も近い流線形リブ14の高さhとは、h
2hとなるように形成されている。すなわち、各流線
形リブ14の高さが増して行く方向と、翼負圧面側前縁
部13cの厚さを増して行く方向とが正反対であるの
で、この前縁部13cの厚さhを含めた断面厚さh
がいずれの箇所でもほぼ等しくなる。このため、軸流送
風機11の樹脂成形時による一体成形の冷却時間の短縮
および肉ひけ等を防止ないし低減することができる。
On the other hand, as shown in FIG.
4 from the boss portion 12 side Ya to the blade outer periphery 13e side Yb
The height h 1 of the streamline rib closest to the blade outer periphery 13 e and the height h 2 of the streamline rib 14 closest to the boss portion 12 are h 1. =
It is formed so as to 2h 2. That is, the direction in which the height of each streamline rib 14 increases and the direction in which the thickness of the blade suction surface side front edge 13c increases are exactly opposite, so that the thickness h 0 of the front edge 13c. cross-sectional thickness h t, including the
Becomes almost equal at any point. For this reason, it is possible to shorten the cooling time of the integral molding due to the resin molding of the axial blower 11 and to prevent or reduce the undercut or the like.

【0037】また、軸流送風機11は以上のように内側
流線形リブ列14bの各流線形リブ14の長手方向の長
さL、設置間隔W、設置位置、前縁の位置、幅Wb、
円弧外面の曲率等をそれぞれ設定したので、縦渦列を翼
負圧面13a上に安定して発生させることができ、その
ために送風音をさらに低減することができる。
As described above, the axial blower 11 has the length L 2 in the longitudinal direction of each streamline rib 14 of the inner streamline rib row 14b, the installation interval W, the installation position, the position of the front edge, the width Wb,
Since the curvature and the like of the outer surface of the circular arc are respectively set, the vertical vortex street can be stably generated on the blade negative pressure surface 13a, so that the blowing noise can be further reduced.

【0038】[0038]

【発明の効果】以上説明したように、本発明は各翼の負
圧面側前縁部に、その前縁端から滑らかに連なる流線形
リブを複数列並設しているので、翼負圧面上にて空気流
れの縦渦列を発生させ、流れの剥離を抑制することがで
き、ひいては翼後縁部後方にできる後流渦幅を小さくし
て送風音を低減することができる。また、各流線形リブ
が流線形状であるので、軸流送風機を例えば樹脂モール
ド成形により簡単に一体成形でき、成形性の向上と製造
コスト低減とを共に図ることができる。
As described above, according to the present invention, a plurality of rows of streamlined ribs that smoothly extend from the leading edge of the blade are arranged side by side on the suction surface side front edge of each blade. , A vertical vortex street of the air flow can be generated, and the separation of the flow can be suppressed. As a result, the wake vortex width formed behind the trailing edge of the blade can be reduced to reduce the blowing noise. In addition, since each streamline rib has a streamline shape, the axial blower can be easily and integrally molded by, for example, resin molding, thereby improving moldability and reducing manufacturing costs.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明の一実施形態に係る軸流送風機を翼負圧
面側から見たときの全体構成の正面図。
FIG. 1 is a front view of the overall configuration of an axial blower according to an embodiment of the present invention when viewed from a blade negative pressure surface side.

【図2】図1で示す軸流送風機の内側流線形リブ列にお
ける各流線形リブの通風側面の傾斜角度を説明するため
の一部切欠正面図。
FIG. 2 is a partially cutaway front view for explaining an inclination angle of a ventilation side surface of each streamline rib in an inner streamline rib row of the axial flow fan shown in FIG.

【図3】図1で示す軸流送風機の内側流線形リブ列にお
ける各流線形リブの傾斜角をそれぞれ変える場合の一部
切欠正面図。
FIG. 3 is a partially cutaway front view in the case of changing the inclination angle of each streamlined rib in the inside streamlined rib row of the axial blower shown in FIG. 1;

【図4】図1等で示す軸流送風機の翼負圧面上の空気流
れの状態を示す一部切欠正面図。
FIG. 4 is a partially cutaway front view showing a state of air flow on a blade negative pressure surface of the axial blower shown in FIG. 1 and the like.

【図5】図4で示す軸流送風機の翼を半径rにて送風
機周方向に沿って切断したときの翼断面図。
[5] blade section view taken along the fan circumferential direction at a radius r 1 wings axial blower shown in FIG.

【図6】図1等で示す軸流送風機の内側流線形リブ列に
おける各流線形リブの長手方向長さと各リブ同士の配置
間隔を示す一部切欠正面図。
FIG. 6 is a partially cutaway front view showing a longitudinal length of each streamlined rib and an arrangement interval between each rib in an inner streamlined rib row of the axial blower shown in FIG. 1 and the like.

【図7】図1等で示す軸流送風機における内側流線形リ
ブ列の各流線形リブを、外側流線形リブ列の各流線形リ
ブ同士の間隙に対応する位置に配置する場合の一部切欠
正面図。
FIG. 7 is a partial cutout in a case where each streamlined rib of the inner streamlined rib row in the axial flow fan shown in FIG. 1 and the like is arranged at a position corresponding to a gap between the streamlined ribs of the outer streamlined rib row; Front view.

【図8】図1等で示す軸流送風機における外側流線形リ
ブ列の各流線形リブの前縁と、内側流線形リブ列の各流
線形リブの前縁の位置関係をそれぞれ示す一部切欠正面
図。
FIG. 8 is a partial cutaway showing the positional relationship between the leading edge of each streamlined rib in the outer streamlined rib row and the leading edge of each streamlined rib in the inner streamlined rib row in the axial blower shown in FIG. Front view.

【図9】図1等で示す軸流送風機における内,外側流線
形リブ列の各流線形リブの幅を説明するための一部切欠
正面図。
FIG. 9 is a partially cutaway front view for explaining the width of each streamline rib of the inner and outer streamline rib rows in the axial blower shown in FIG. 1 and the like.

【図10】図1等で示す各流線形リブの縦断面図。FIG. 10 is a longitudinal sectional view of each streamline rib shown in FIG. 1 and the like.

【図11】図1等で示す軸流送風機の前縁部の送風機半
径方向に沿う断面図。
11 is a cross-sectional view of a front edge portion of the axial blower shown in FIG. 1 and the like, taken along a radial direction of the blower.

【図12】図1等で示すボス部と内側流線形リブ列とを
送風機半径方向に沿って切断したときの断面を示す模式
図。
FIG. 12 is a schematic diagram showing a cross section when the boss portion and the inner streamline rib row shown in FIG. 1 and the like are cut along the radial direction of the blower.

【図13】従来の軸流送風機の負圧面側から見たときの
正面図。
FIG. 13 is a front view of a conventional axial blower as viewed from a negative pressure side.

【図14】図13で示す従来の軸流送風機の翼1枚分を
示す一部切欠正面図。
FIG. 14 is a partially cutaway front view showing one blade of the conventional axial flow fan shown in FIG.

【図15】図13で示す軸流送風機の回転中心から任意
の半径で翼を周方向に切断したときの翼断面図。
FIG. 15 is a cross-sectional view of the blade when the blade is circumferentially cut at an arbitrary radius from the rotation center of the axial blower shown in FIG. 13;

【符号の説明】[Explanation of symbols]

11 軸流送風機 12 ボス部 13 翼 13a 翼の負圧面 13c 翼の前縁部 13d 翼の後縁部 13e 翼の外周端部 14 流線形リブ 14a 外側流線形リブ列 14b 内側流線形リブ列 15a,15b 外,内側円弧曲線 Reference Signs List 11 axial flow blower 12 boss portion 13 blade 13a suction surface of blade 13c leading edge of blade 13d trailing edge of blade 13e outer peripheral end of blade 14 streamlined rib 14a outer streamlined rib row 14b inner streamlined rib row 15a, 15b Outer and inner arc curves

Claims (9)

【特許請求の範囲】[Claims] 【請求項1】 回転軸が固定されるボス部の外周に、複
数の翼を配設した軸流送風機において、 上記各翼の負圧面側前縁部に、その前縁から翼後縁に向
けて滑かに連なる流線形リブの複数を、送風機半径方向
に所定の間隔を置いて上記前縁の輪郭線に沿って列状に
配設し、この流線形リブ列を送風機周方向に所定の間隔
を置いて複数列設けたことを特徴とする軸流送風機。
1. An axial flow blower having a plurality of blades disposed on an outer periphery of a boss portion to which a rotating shaft is fixed, wherein: a front surface of each of the blades has a suction surface side; A plurality of streamlined ribs that are smoothly connected are arranged in a row along the contour of the front edge at predetermined intervals in the radial direction of the blower, and the streamlined rib rows are arranged in a predetermined manner in the circumferential direction of the blower. An axial blower characterized by having a plurality of rows provided at intervals.
【請求項2】 翼前縁側の外側流線形リブ列よりも送風
機周方向内側に設けた内側流線形リブ列の各流線形リブ
は、その流入空気の通風方向を案内する通風側面の角度
θaを、上記外側流線形リブ列の通風側面の角度θbに
対して12°〜18°の範囲で傾斜させていることを特
徴とする請求項1記載の軸流送風機。
2. Each streamlined rib of an inner streamlined rib array provided on the inner side in the blower circumferential direction with respect to the outer streamlined rib array on the blade leading edge side has an angle θa of a ventilation side surface for guiding the direction of airflow of the inflow air. 2. The axial flow blower according to claim 1, wherein said outer streamlined rib row is inclined at an angle of 12 [deg.] To 18 [deg.] With respect to the angle [theta] b of the ventilation side surface.
【請求項3】 内側流線形リブ列の各流線形リブは、回
転軸中心Oと、翼外周と翼後縁との交点Qと、を結ぶ線
分OQに対して各々の所定角度でそれぞれ傾斜させ、こ
れらの各傾斜角を翼外周からボス部側の流線形リブに行
くに従って大きくすることを特徴とする請求項1または
2記載の軸流送風機。
3. Each streamline rib of the inner streamline rib row is inclined at a predetermined angle with respect to a line segment OQ connecting the rotation axis center O and an intersection Q between the blade outer periphery and the blade trailing edge. 3. The axial flow blower according to claim 1, wherein each of the inclination angles increases from the blade outer periphery to the streamline rib on the boss portion side.
【請求項4】 内側流線形リブ列は、その各流線形リブ
を送風機半径方向に等間隔で配置する一方、これらの各
流線形リブの送風機周方向に沿う長さLを、外側流線
形リブ列の各流線形リブの送風機周方向に沿う長さL
に対し、ほぼ0.8Lの長さに形成していることを特
徴とする請求項1〜3のいずれか1項に記載の軸流送風
機。
Wherein the inner flow linear ribs column while arranged at equal intervals each of its streamlined ribs blower radially, the length L 2 along the blower circumferential direction of each of these aerodynamic ribs, outer streamlined the length L 1 along the fan circumferential direction of the aerodynamic ribs of the rib row
Relative, axial flow fan according to claim 1, characterized in that it is formed almost the length of 0.8 L 1.
【請求項5】 内側流線形リブ列は、その流線形リブ
を、外側流線形リブ列の流線形リブ同士の間隙に対応す
る位置に配設していることを特徴とする請求項1〜4の
いずれか1項に記載の軸流送風機。
5. The inner streamlined rib array, wherein the streamlined ribs are arranged at positions corresponding to the gaps between the streamlined ribs of the outer streamlined rib array. The axial flow blower according to any one of the above.
【請求項6】 内側流線形リブ列の各流線形リブは、そ
の送風機周方向各前縁を、外側流線形リブ列の各流線形
リブの送風機周方向各前縁を結ぶ円弧曲線の中心をP、
その半径をrとしたときに、その中心Pと同心でかつ
半径rよりも大きい半径rの円弧線上に位置させて
いることを特徴とする請求項1〜5のいずれか1項に記
載の軸流送風機。
6. Each streamline rib of the inner streamline rib row has a center of an arc curve connecting each front edge of the streamer ribs of the outer streamline rib row in the fan circumferential direction. P,
The radius is taken as r 1, to any one of claims 1 to 5, characterized in that it is positioned on the center P and concentric with and arc lines of the large radius r 2 than the radius r 1 An axial blower as described.
【請求項7】 内,外両側の流線形リブ列の各流線形リ
ブは、その送風機半径方向に沿う幅がみなほぼ同一幅に
形成されていることを特徴とする請求項1〜6のいずれ
か1項に記載の軸流送風機。
7. The streamlined ribs of the inner and outer streamlined rib rows are formed to have substantially the same width along the radial direction of the blower. 2. The axial blower according to claim 1.
【請求項8】 内側流線形リブ列の各流線形リブは、そ
の送風機周方向に沿う断面の外面が円弧面をなし、その
円弧外面の翼前縁側一部の円弧曲面の半径Raの方が、
その反対側他部の円弧曲面の半径Rbよりも大きくなる
ように一体に形成されていることを特徴とする請求項1
〜7のいずれか1項に記載の軸流送風機。
8. Each of the streamline ribs of the inner streamline rib row has an outer surface having a circular cross section along a circumferential direction of the blower, and a radius Ra of a circular arc surface of a part of the circular outer surface on the blade leading edge side is larger. ,
2. The structure as claimed in claim 1, wherein said second portion is integrally formed so as to be larger than a radius Rb of the arcuate curved surface at the other portion on the opposite side.
The axial blower according to any one of claims 1 to 7.
【請求項9】 内側流線形リブ列の各流線形リブは、そ
の翼厚方向に沿う断面高さを、ボス部側から翼外周方向
に行くに従って漸次薄くなる翼前縁部断面の厚さとは逆
にボス部側から翼外周側に行くに従って漸次高くなるよ
うに除変させると共に、上記翼外周に最も近い流線形リ
ブの高さをhとし、上記ボス部に最も近い流線形リブ
の高さをhとしたときに、h=2hとなるように
設定されていることを特徴とする請求項1〜8のいずれ
か1項に記載の軸流送風機。
9. Each of the streamline ribs of the inner streamline rib row has a cross-sectional height along the blade thickness direction which is gradually reduced from the boss portion side toward the blade outer peripheral portion. with removal strange is allowed to become gradually higher toward the boss portion side blade outer peripheral side Conversely, the height of the nearest streamlined rib to the wing outer periphery and h 1, the closest streamlined ribs to the boss height of a is taken as h 2, axial flow fan according to any one of claims 1-8, characterized in that it is set such that h 1 = 2h 2.
JP26737099A 1999-09-21 1999-09-21 Axial blower Expired - Lifetime JP4321690B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP26737099A JP4321690B2 (en) 1999-09-21 1999-09-21 Axial blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP26737099A JP4321690B2 (en) 1999-09-21 1999-09-21 Axial blower

Publications (2)

Publication Number Publication Date
JP2001090692A true JP2001090692A (en) 2001-04-03
JP4321690B2 JP4321690B2 (en) 2009-08-26

Family

ID=17443903

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
JP (1) JP4321690B2 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005052377A1 (en) * 2003-11-27 2005-06-09 Daikin Industries, Ltd. Blade wheel for centrifugal blower and centerifugal blower with the same
KR100713996B1 (en) * 2003-11-27 2007-05-04 다이킨 고교 가부시키가이샤 Blade wheel for centrifugal blower and centrifugal blower with the same
US8007240B2 (en) 2003-11-27 2011-08-30 Daikin Industries, Ltd. Impeller of centrifugal fan and centrifugal fan disposed with the impeller
JP2008038698A (en) * 2006-08-03 2008-02-21 Shin Meiwa Ind Co Ltd Impeller and submerged mixer
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WO2015029245A1 (en) * 2013-09-02 2015-03-05 三菱電機株式会社 Propeller fan, air-blowing device, and outdoor unit
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CN116783394B (en) * 2021-01-21 2024-04-26 大金工业株式会社 Axial fan and air conditioner

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